contributor author | Reza | |
contributor author | Jamilnia | |
contributor author | Abolghasem | |
contributor author | Naghash | |
date accessioned | 2017-05-08T21:33:57Z | |
date available | 2017-05-08T21:33:57Z | |
date copyright | October 2013 | |
date issued | 2013 | |
identifier other | %28asce%29as%2E1943-5525%2E0000194.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/56344 | |
description abstract | In this paper, a general guidance method based on a receding horizon control technique and online trajectory optimization is proposed for various interception problems. In this method, the interception problem is defined as an optimal control problem by full dynamics of the interceptor and the current position and velocity of the target in the three-dimensional space. By solving the interception optimal control problem for various objective and constraint functions, integrated guidance and control commands are generated online during interception. To find the closed-loop and state-dependent solution, the interception optimal control problem is defined in a receding horizon control framework. To quickly solve the interception problem, the direct trajectory optimization method, which is a combination of a differential flatness concept, | |
publisher | American Society of Civil Engineers | |
title | Optimal Guidance Based on Receding Horizon Control and Online Trajectory Optimization | |
type | Journal Paper | |
journal volume | 26 | |
journal issue | 4 | |
journal title | Journal of Aerospace Engineering | |
identifier doi | 10.1061/(ASCE)AS.1943-5525.0000194 | |
tree | Journal of Aerospace Engineering:;2013:;Volume ( 026 ):;issue: 004 | |
contenttype | Fulltext | |